METHOD FOR UTILIZATION OF CHARGES OF COMPOSITE SOLID PROPELLANT BASED ON AMMONIUM PERCHLORATE

摘要

The invention relates to rocket engineering, in particular to the utilization of charges of solid propellants based on ammonium perchlorate. The aim of the invention is to improve the environmental performance while maintaining the fractional composition of the fuel and increase vzryvobezrpasnosti. The objective is achieved due to the fact that in the proposed method, the charge is degraded by subjecting it to heat flow capacity of no less tfee 2 -105 W / m2. when this is generated, and then evacuating the vacuum is maintained not higher than 2.10 Pa, and the collection of solid decomposition products ultrasonic generation is performed. 1 ZP f -ly 5 yl.